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author:

Yuan, Yuan (Yuan, Yuan.) [1] | Zhang, Tianhong (Zhang, Tianhong.) [2] | Lin, Zhonglin (Lin, Zhonglin.) [3] (Scholars:林忠麟) | Zhao, Zhiwen (Zhao, Zhiwen.) [4] | Zhang, Xinglong (Zhang, Xinglong.) [5]

Indexed by:

SCIE

Abstract:

This paper presents a fault tolerant control (FTC) design for the actuator faults in a variable cycle engine (VCE). Ensured by the multiple variable geometries structure of VCE, the design is realized by distributing the control effort among the unfaulty actuators with the "functional redundancy" idea. The FTC design consists of two parts: the fault reconstruction part and the fault tolerant control part, which use a sliding mode observer (SMO) and a sliding mode control (SMC) scheme respectively. Considering the inaccuracy of the fault reconstruction result, the proposed design requires only inaccurate fault information. The stability of the closed-loop control system is proved and the existence condition for the proposed control law is analyzed. This work also reveals its relation to the sliding mode control allocation design and the adaptive SMC design. An application case is then studied for tolerating the loss of effectiveness fault of the nozzle area actuator. Results show that the FTC design is able to tolerate the fault and achieves the same control goal as in the fault-free situation. Finally, a hardware-in-the-loop test is carried out to verify the design in a real-time distributed control system, which demonstrates its use from the engineering perspective.

Keyword:

aircraft engine control allocation fault tolerant control hardware-in-the-loop test sliding mode control

Community:

  • [ 1 ] [Yuan, Yuan]Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
  • [ 2 ] [Zhang, Tianhong]Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
  • [ 3 ] [Zhang, Xinglong]Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
  • [ 4 ] [Lin, Zhonglin]Fuzhou Univ, Sch Mech Engn & Automat, Fuzhou 350116, Peoples R China
  • [ 5 ] [Zhao, Zhiwen]Cranfield Univ, Sch Aerosp Transport & Mfg, Ctr Prop Engn, Cranfield MK43 0AL, Beds, England

Reprint 's Address:

  • [Zhang, Tianhong]Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China

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Source :

ACTUATORS

ISSN: 2076-0825

Year: 2021

Issue: 2

Volume: 10

2 . 5 2 3

JCR@2021

2 . 2 0 0

JCR@2023

ESI Discipline: ENGINEERING;

ESI HC Threshold:105

JCR Journal Grade:2

CAS Journal Grade:4

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count: 4

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 2

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